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Nonlinear Tollmien-Schlichting/vortex interaction in boundary layersThe nonlinear reaction between two oblique 3-D Tollmein-Schlichting (TS) waves and their induced streamwise-vortex flow is considered theoretically for an imcompressible boundary layer. The same theory applies to the destabilization of an incident vortex motion by subharmonic TS waves, followed by interaction. The scales and flow structure involved are addressed for high Reynolds numbers. The nonlionear interaction is powerful, starting at quite low amplitudes with a triple-deck structure for the TS waves but a large-scale structure for the induced vortex, after which strong nonlinear amplification occurs. This includes nonparallel-flow effects. The nonlinear interaction is governed by a partial differential system for the vortex flow coupled with an ordinary-differential one for the TS pressure. The solution properties found sometimes produce a breakup within a finite distance and sometimes further downstream, depending on the input amplitudes upstream and on the wave angles, and that then leads to the second stages of interaction associated with higher amplitudes, the main second stages giving either long-scale phenomena significantly affected by nonparallelism or shorter quasi-parallel ones governed by the full nonlinear triple-deck response.
Document ID
19880020331
Acquisition Source
Legacy CDMS
Document Type
Preprint (Draft being sent to journal)
Authors
Hall, P.
(Exeter Univ. (England), United States)
Smith, F. T.
(University Coll. London, United Kingdom)
Date Acquired
September 5, 2013
Publication Date
August 1, 1988
Subject Category
Aeronautics (General)
Report/Patent Number
NASA-CR-181698
ICASE-88-46
NAS 1.26:181698
Accession Number
88N29715
Funding Number(s)
CONTRACT_GRANT: NAS1-18107
PROJECT: RTOP 505-90-21-01
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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